ATE487658T1 - SEALING DEVICE FOR THE HULL THROUGH OF AN ACTUATING AXIS OF A FLAPS GUIDE - Google Patents

SEALING DEVICE FOR THE HULL THROUGH OF AN ACTUATING AXIS OF A FLAPS GUIDE

Info

Publication number
ATE487658T1
ATE487658T1 AT05078055T AT05078055T ATE487658T1 AT E487658 T1 ATE487658 T1 AT E487658T1 AT 05078055 T AT05078055 T AT 05078055T AT 05078055 T AT05078055 T AT 05078055T AT E487658 T1 ATE487658 T1 AT E487658T1
Authority
AT
Austria
Prior art keywords
sealing device
hull
hollow bodies
flap
actuating axis
Prior art date
Application number
AT05078055T
Other languages
German (de)
Inventor
Gomez Ignacio Zamora
Original Assignee
Airbus Operations Sl
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=35840617&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ATE487658(T1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Airbus Operations Sl filed Critical Airbus Operations Sl
Application granted granted Critical
Publication of ATE487658T1 publication Critical patent/ATE487658T1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof

Abstract

Sealing device for the flap track for the flap-actuating shaft, in the belly fairing of an aircraft, with a top hollow body 1 and a bottom hollow body 7 which are flexibly compressible, each comprising at least one interior chamber 2, 8 with open sides 2a, 2b, a wall 3, 9 with respective external contact surfaces 3a which are in flexible contact with each other, the outer surfaces 4a, 10a of the front walls 4, 10 of the hollow bodies 1, 7 jointly forming an outer sealing surface 11 which covers the flap track 19, said hollow bodies 1,7 having jointly a vertical compression flexibility such that the contact surfaces 3a, 9a retract around the actuating shaft 20, the interior chambers 2, 8 extending between the front walls 4, 10 and rear walls 5, 11 of the hollow bodies 2, 7.
AT05078055T 2004-12-31 2005-12-28 SEALING DEVICE FOR THE HULL THROUGH OF AN ACTUATING AXIS OF A FLAPS GUIDE ATE487658T1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200500028A ES2310059B1 (en) 2004-12-31 2004-12-31 SEALING DEVICE FOR THE PASSING SLOT OF THE FLAP DRIVE TREE IN THE VENTRAL SIDE OF AN AIRPLANE.

Publications (1)

Publication Number Publication Date
ATE487658T1 true ATE487658T1 (en) 2010-11-15

Family

ID=35840617

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05078055T ATE487658T1 (en) 2004-12-31 2005-12-28 SEALING DEVICE FOR THE HULL THROUGH OF AN ACTUATING AXIS OF A FLAPS GUIDE

Country Status (8)

Country Link
US (1) US7422177B2 (en)
EP (1) EP1676773B1 (en)
AT (1) ATE487658T1 (en)
BR (1) BRPI0600154B1 (en)
CA (1) CA2531700C (en)
DE (1) DE602005024658D1 (en)
EA (1) EA009543B1 (en)
ES (1) ES2310059B1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7744034B2 (en) * 2007-07-27 2010-06-29 The Boeing Company Translating flap drive door
GB0800770D0 (en) 2008-01-17 2008-02-27 Airbus Uk Ltd Aerofynamic sealing member for aircraft
FR2953193B1 (en) * 2009-11-30 2012-03-16 Airbus Operations Sas AIRCRAFT COMPRISING AN INTERNAL ROOFING
US10501166B2 (en) 2012-09-20 2019-12-10 The Boeing Company Methods and apparatus to control a gap between movable aircraft wing components
US9688384B1 (en) * 2012-09-20 2017-06-27 The Boeing Company Methods and apparatus to control a gap between movable aircraft wing components
US9623957B2 (en) * 2014-08-26 2017-04-18 The Boeing Company Torque tube door
BE1024611B1 (en) * 2017-01-24 2018-04-24 Sonaca S.A. AIRCRAFT ASSEMBLY COMPRISING A SOLIDARITY JOINT MOBILE SHUTTER OF A SHAFT THROUGH A FUSELAGE OPENING EQUIPPED WITH AN IMPROVED SEALING DEVICE
US10793252B2 (en) * 2018-03-30 2020-10-06 The Boeing Company Apparatus and method for covering an opening in an aircraft
CN114616174A (en) * 2019-10-31 2022-06-10 空中客车德国运营有限责任公司 Baffle assembly and baffle arrangement for shielding a trunnion opening, and high lift system and aircraft equipped therewith
CN112722241B (en) * 2021-02-02 2024-04-12 中国空气动力研究与发展中心空天技术研究所 Telescopic belly flap

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2405726A (en) * 1940-08-14 1946-08-13 Edward F Zap Airplane wing construction
SU67249A1 (en) * 1945-04-06 1945-11-30 А.И. Лисичкин Fowler type flap control device
US3031198A (en) * 1957-05-16 1962-04-24 Raymond A Hudson Liquid seal for movable members
US2984506A (en) * 1957-07-02 1961-05-16 Remi J Gits Jr Boot seal
GB1144231A (en) * 1966-07-07 1969-03-05 British Aircraft Corp Ltd Improvements relating to aircraft having variable sweep-back wings
US3486720A (en) * 1967-12-07 1969-12-30 Boeing Co Continuous slot forming leading edge slats for cranked wings
DE2011345A1 (en) * 1970-03-10 1971-09-23 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Device for covering a wall gap in aircraft fuselages or the like.
US3917194A (en) * 1971-09-13 1975-11-04 Messerschmitt Boelkow Blohm Automatically operating device for sealing a fuselage recess of aircrafts
GB1508788A (en) * 1975-05-03 1978-04-26 Pitcraft Ltd Electric power supply track
US4434959A (en) * 1981-09-28 1984-03-06 The Boeing Company Airfoil flap assembly with flap track member
DE3276631D1 (en) * 1982-12-06 1987-07-30 Boeing Co Wing trailing edge air dams
US4576347A (en) * 1984-10-30 1986-03-18 The Boeing Company Flap torque tube slot seal
GB8821220D0 (en) * 1988-09-09 1988-12-14 British Aerospace Fuselage mounted flap drive for wing trailing edge flaps
US5161757A (en) * 1989-07-31 1992-11-10 The Boeing Company Extending bent shaft flap drive
US5458343A (en) * 1994-08-11 1995-10-17 General Electric Company Aircraft engine firewall seal
US5839698A (en) * 1997-10-23 1998-11-24 Northrop Grumman Corporation Control surface continuous seal
US6299108B1 (en) * 1997-12-12 2001-10-09 Jeffrey V. Lindstrom Method and apparatus for detecting skew and asymmetry of an airplane flap

Also Published As

Publication number Publication date
CA2531700A1 (en) 2006-06-30
CA2531700C (en) 2012-01-10
EP1676773A1 (en) 2006-07-05
BRPI0600154B1 (en) 2018-12-26
BRPI0600154A (en) 2006-09-19
EA200501933A3 (en) 2006-12-29
EA009543B1 (en) 2008-02-28
US20060145013A1 (en) 2006-07-06
ES2310059A1 (en) 2008-12-16
DE602005024658D1 (en) 2010-12-23
ES2310059B1 (en) 2009-11-11
EP1676773B1 (en) 2010-11-10
EA200501933A2 (en) 2006-08-25
US7422177B2 (en) 2008-09-09

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Legal Events

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